JASC 5754
Service difficulty reports · 17,348
Reports filed under 5754 · Leading Edge Devices, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5754' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5754' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS203495Bullnose · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND NR 2 K-FLAP BULLNOSE AROUND LOWER ATTACH POINT HAS CORROSION. REPLACED K-FLAP IAW SRM 57-50-1, 51-30-2, OHM 57-51-11, 20-20-00, M/M 27-81-00.SDR UPS203494Bullnose · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND NR 3 K-FLAP BULLNOSE I/B LOWER ADJUSTMENT ROD ATTACH POIINT CORRODED. REPLACED K-FLAP IAW SRM 57-50-1, 51-30-2, OHM 57-51-11.SDR DL72K952534Skin · crackedFOUND DURING A-2 LETTER CHECK - NR 2 L/E SLAT LOWER FORWARD SKIN ATTACH ANGLE CRACKED UNDER ANTI-ICE DUCT. REPAIRED PER MM 57-54-0, PG 807A.SDR DL72K952533Skin · crackedFOUND DURING A-2 LETTER CHECK- .50 INCH CRACK COVESKIN ATTACH ANGLE BELOW I/B STOP PAD NR 8 SLAT, 1 INCH CRACK COVESKIN ATTACH ANGLE BELOW O/B STOP PAD NR 8 SLAT. REPAIRED BOTH CRACKS PER MM 57-54-0, PG 807.SDR DL72K952532Skin · crackedFOUND DURING A-2 LETTER CHECK - .50 INCH CRACK COVESKIN ATTACH ANGLE UNDER I/B STOP PAD NR 7 SLAT. REPAIRED PER MM 57-54-0 OG 807.ER M/M 57-54-0 P807.SDR DL72K952531Skin · crackedFOUND DURING A-2 LETTER CHECK - .25 INCH CRACK COVESKIN ATTACH ANGLE NR 6 SLAT BELOW TAI DUCT. REPAIRED PER MM 57-54-0, PG 807.SDR UPS203486Skin · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND RT WING NR 6 K-FLAP BULLNOSE O/B HINGE UPPER SURFACE OF UPPER ATTACH POINTS HAVE CORROSION. INSTALLED FABRICATED PARTS IAW SRM 57-50-1, 51-10-6, 51-10-1, 51-20-04.SDR DL767952519Te Wedge · dentedTRAILING EDGE WEDGE HAD HAIL DAMAGE. REPLACED WEDGE PER CMM 57-43-37. REPAIRS ACCOMPLISHED DURING SHOP VISIT FOR NR 6 L/E SLAT PANEL.SDR DL72W952512Web · crackedNR 6 SLAT O/B ACT ROD END WEB CRACKED AFT SIDE. FOUND AT B-2 LTR CK. REPAIRED PER SRM 57-54-0.SDR DL72W952511Angle · crackedNR 2 SLAT I/B STOP PAD LWR ATTACH ANGLE IS CRACKED. FOUND AT B-2 LTR CK. REPAIRED PER MM 57-54-0.SDR UPS203457K-Flap · corrosionWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP. REPLACED IAW M/M 27-81-1.SDR UPS203450K-Flap · corrodedWHILE IN C-CHECK MAINTENANCE FOUND CORROSION ON NR 2 K-FLAP. REPLACED IAW M/M 27-81-1.SDR UPS203449K-Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 K-FLAP. REPLACED IAW M/M 27-81-1.SDR DL72S952493Angle · cracked1.25 INCH CRACK IN NR 7 SLAT ACT I/B ATTACH FITTING, AFT OF UPPER MOUNT BOLT ON WING FRONT SPAR. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-42-0.SDR DL72S952491Angle · crackedANGLE CRACKED .50 INCH BELOW TAI DUCT ON NR 3 SLAT. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0 PG 807.SDR DL72S952490Fairing · crackedNR 5 SLAT I/B TRACK FAIRING CRACKED. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0 PG 820.SDR DL72S952489Rib · cracked1) NR 7 SLAT ACT ROD END WEB CRACKED I/B AFT SIDE. 2) NR 7 SLAT ACT ROD END WEB CRACKED O/B AFT SIDE. FOUND DURING C-1 LTR CK. REPAIRED BOTH ITEMS PER MM 57-54-0 PAR 3B.SDR DL72S952483Flap · crackedPREVIOUS REPAIR CRACKED AT CENTER ATTACH POINT FOR BULLNOSE, 36 INCHES FROM INBD END, OF NR 5 L/E KRUGER FLAP. REPAIRED PER SRM 57-50-3, FIG. 11 REFERENCE ERA NR 270969-14.SDR DL757952603Te Wedge · wornT/E WEDGE WORN BOTTOM SIDE 36 INCHES FROM I/B END OF NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02, DURING SHOP VISIT.SDR DL72L952471Rib · crackedTHE NR 7 SLAT ACTUATOR ATTACH NOSE RIB LWR SIDE AFT CRACKED .5 INCH. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0 PAR 3B.SDR DL72L952470Angle · crackedA .5 INCH CRACK NR 3 SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER M/M 57-54-0 PG 807A.SDR DL72L952469Angle · crackedNR 7 SLAT COVE SKIN ATTACH ANGLE UNDER TAI DUCT CRACKED 1 INCH. FOUND DURING A-1 LTR CK TPAMM. REPAIRED PER MM 57-54-0 PG 807A.SDR DL72E952417Slat · crackedFOUND DURING F-1 LETTER CHECK, .75 INCH CRACK AT NR 7 SLAT UNDER I/B STOP FITTING. REPAIRED PER MM 57-54-0.SDR DL72E952416Skin · crackedFOUND DURING F-1 LETTER CHECK, .375 INCH CRACK ON COVE SKIN SUPPORT ANGLE, NR 7 SLAT AT THERMAL ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.SDR CAL950508Ribs · crackedGSO - INSPECTION FOUND 2 LOWER LEADING EDGE INBOARD SLAT RIBS CRACKED AT ACTUATOR. THE CRACKS WERE APPROXIMATELY .75 INCH LONG. THE CRACKS WERE STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 57-30-3 AND SRM 51-30-2. (X)SDR CAL950502Rib · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF THE NR 3 SLAT OUTBOARD TRACK OUTBOARD RIB. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 57-50-3, SRM 51-40-3, AND SRM 51-30-2. (X)SDR CAL950501Rib · crackedGSO - INSPECTION FOUND A 2.25 INCH CRACK IN RADIUS OF NR 3 SLAT INBOARD TRACK INBOARD RIB. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 57-30-2 AND SRM 51-30-2. (X)SDR 95ZZZM117Rivet · poppedRIVET HEAD POPPED ON FORWARD SPAR CAP AFT OF NR 9 SLAT (INBOARD END). REPLACED RIVET PER BOEING SRM 51-30-03. (M)SDR UPS203425Channel · crackedWHILE IN SI CHECK MAINTENANCE FOUND NR 2 K-FLAP O/B ACTUATOR SUPPORT CHANNEL CRACKED. INSTALLED FABRICATED PARTS IAW SRM 57-20-2, 51-20-1, 51-30-2, M/M 20-50-21.SDR UPS203424Flap · corrodedWHILE IN SI CHECK MAINTENANCE FOUND NR 2 K-FLAP HAS CORROSION. REMOVED AND REPLACED NR 2 K-FLAP IAW M/M 27-81-01.SDR DL757952371Te Wedge · delaminatedDURING SHOP INSPECTION, NR 5 L/E SLAT WAS FOUND WITH DELAMINATION TO TRAILING EDGE WEDGE. REPLACED WEDGE PER SRM 57-43-02.SDR UPS203409Skin · crackedWHILE IN SI CHECK, MAINTENANCE FOUND NR 2 SLAT HAS 2 GOUGES ON T/E ABOVE THE I/B GUIDE HOOK. REPLACED SLAT IAW B727-5750-1235.SDR DL72W952363Slat · crackedFOUND DURING E-1 LETTER CHECK - .25 INCH CRACK AT NR 7 SLAT O/B STOP PAD BELOW COVE PNL. REPAIRED PER MM 57-54-0.SDR DL72W952362Rib · crackedFOUND DURING E-1 LETTER CHECK - .1875 INCH CRACK BOTTOM OF NOSE RIB JUST LEFT OF SLAT ACTUATOR ROD END ON NR 4 SLAT. ONE INCH CRACK ON NR 4 SLAT I/B TRACK LOWER FAIRING RADIUS. BOTH REPAIRED PER MM 57-54-0.SDR DL72W952361Slat · crackedFOUND DURING E-1 LETTER CHECK - .50 INCH CRACK AT I/B STOP PAD ON NR 2 SLAT. REPAIRED PER MM 57-54-0.SDR DL72E952501Attach Bracket · crackedFOUND ON CV2 CHECK NR 2 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED. REPAIR: REPAIRED PER M/M 57-20-21.SDR DL72E952880Skin · oil cannedOUTER SKIN OIL CANNING AND DENTED 58 INCHES FROM IB END. REPAIRED AS PER 57-50-03 FIG 1 AND IN REFERENCE TO ERA NR 271165-14 FOR NR 5 L/E SLAT, DURING SHOP INSPECTION.SDR AALA951008Skin · damagedSFO - FLT NR 682 - NR 4 SLAT LEADING EDGE HAS LARGE HOLE, NOTICED BY PASSENGER AFTER TAKEOFF AND CLIMB. NOTIFIED COCKPIT OF HOLE IN LEFT SLAT AND WAS CONFIRMED BY FLIGHT OFFICER. NO VIBRATION OR UNUSUAL FLIGHT CONTROL PRESSURE WAS FELT. ON LANDING WHEN FLAPSSDR SWAA950430Skin · crackedDURING SCHEDULED TRANSITION CHECK, FOUND NR 5 SLAT SKIN LOWER T/E SKIN CRACKED. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND DRAWING BAC 65C30133.SDR MWEA95209Skin · crackedDURING ROUTINE INSPECTION, 2 - 3 INCH CRACKS WERE FOUND ON THE RT NR 2 SLAT APPROX 8 INCHES APART, UNDERSIDE OF SLAT. MAINTENANCE STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER IAW SRM 57-10-1 AND 51-10-3. RETURNED AC TO SERVICE.SDR DL757952322Te Wedge · delaminatedT/E WEDGE DELAMINATED. COMPLIED WITH AD 90-23-06 PER SRM 57-54-02 FIG 202, FOR NR 2 L/E SLAT AT SHOP INSPECTION.SDR DL72S952298Skin · crackedNR 6 L/E FLAP HAD A PREVIOUS REPAIRED CRACK WHICH CRACKED FURTHER. REPAIRED PER SRM 57-50-3, FOUND AT HMV.SDR DL72S952297Skin · crackedNR 6 L/E FLAP HAD A CRACK AT I/B HINGE FITTING AFT END. REPAIRED PER SRM 57-50-03 PG 32.SDR P5CA9500149Skin · damagedTOP EDGES OF EACH LEFT WING LEADING EDGE FLAP NR 1 TO NR 10 ARE DAMAGED. REPAIRED PER BOEING SRM 51-40-09.SDR DL72L952294Rib · crackedUPON INSPECTION, RIB NR 11 FOUND CRACKED IN LWR FWD CORNER. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT.SDR DL72L952293Rib · crackedUPON INSPECTION, A CRACK WAS FOUND IN THE LOWER FWD CORNER OF NR 10 RIB. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT.SDR DL72L952292Heat Shield · crackedUPON INSPECTION, A CRACK WAS FOUND IN HEAT SHIELD BETWEEN RIBS 11 AND 12, AND BETWEEN RIBS 12 AND 13. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT.SDR UPS203391Bull Nose · corrodedWHILE IN SI CHECK, MAINTENANCE FOUND ATTACH POINTS BONDING JUMPERS ON NR 4 K-FLAP AND BULL NOSE OUTER LOWER SIDE HAS CORROSION. REPAIRED K-FLAP IAW 727-57-1370.SDR UPS203384Fittings · corrodedWHILE IN SI CHECK, MAINTENANCE FOUND CORROSION IN BORE OF TRACK ATTCH RIB FITTINGS O/B AND I/B OF NR 3 SLAT. INSTALLED NEW FITTINGS IAW SRM 51-30-02.SDR UPS203383Fitting · corrodedWHILE IN SI CHECK, MAINTENANCE FOUND CORROSION IN BORE OF TRACK ATTCH RIB FITTINGS O/B AND I/B OF NR 8 SLAT. INSTALLED NEW FITTINGS IAW SRM 51-30-02.
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